▸Orbital parameters

Orbit class	SSO
Inclination	97.7566°
Eccentricity	0.0003131
Period	96.5 min
Apogee	595 km
Perigee	591 km
Mean motion	14.91694075 rev/day
RAAN	145.7085°
Arg of perigee	23.9959°
Mean anomaly	336.1405°
B*	3.2305e-4
Rev at epoch	1,465

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 68491U 26067CD 26187.86422215 .00003194 00000-0 32305-3 0 9996

2 68491 97.7566 145.7085 0003131 23.9959 336.1405 14.91694075 14659

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-DELOITTE-2",
  "OBJECT_ID": "2026-067CD",
  "EPOCH": "2026-07-06T20:44:28.794+00:00",
  "MEAN_MOTION": 14.91694075,
  "ECCENTRICITY": 0.0003131,
  "INCLINATION": 97.7566,
  "RA_OF_ASC_NODE": 145.7085,
  "ARG_OF_PERICENTER": 23.9959,
  "MEAN_ANOMALY": 336.1405,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68491,
  "REV_AT_EPOCH": 1465,
  "BSTAR": 0.00032305,
  "MEAN_MOTION_DOT": 0.00003194,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	LEMUR-2-DELOITTE-2
Operator	Deloitte Space, El Segundo / SpireHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Mar 30, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/68491

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.